Cover Image

Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /

Bibliographic Details
Main Author: Hall, Robert M. (Author)
Corporate Author: Langley Research Center
Format: Government Document eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, April 1979.
Series:NASA technical paper ; 1385.
Subjects:
Airfoils.
Cryogenic wind tunnels.
Pressure distribution.
Stagnation temperature.
Supercooling.
Online Access:https://purl.fdlp.gov/GPO/gpo70962
Description
Item Description:Title from title screen (viewed on Aug. 10, 2016).
"April 1979."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (69 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 22-23).